книги / Английский язык
..pdftanks; 5. an auxiliary assembly; 6. a solid propellant; 7. in respect to the size of the airframe; 8. to impart the propulsive thrust to the payload; 9. to assemble the airframe; 10. an integral part of the re-entry body; 11. to perform the guidance; 12. the use of an oxidizer; 13. whether liquid or solid
45. Прочтите и переведите без словаря:
1. We consider the re-entry body to be a main subsystem of the ballistic missile. 2. The re-entry body is to move towards the target. 3. The control signals are generated as a result of com mands from a guidance system. 4. An auxiliary power supply is
to give electric energy to various devices. 5. We know the mainstructure of the missile to be called the airframe. 6. The task of the student was to assemble and disassemble a pump. 7. You should know each stage of the two-stage liquid propellant vehicle to contain a rocket engine and two storage tanks. 8. The engineers consider a propulsive system to be a main part of the missile. 9. The combustion gases leave the engine through the exhaust nozzle. 10. The steering device is an integral part of any guided missile.
46. Найдите в тексте "Components of the Ballistic Missile" ответы на вопросы:
1. How is the airframe of the ballistic missile defined?
2.What does a turbopump assembly do?
3.What do the turbopump assemblies consist of? •4. How is the missile controlled in flight?
5. What signals |
are generated as a result of commands from |
a guidance system? |
|
6.Do you know the re-entry body to contain the warhead, the fuze and the arming mechanism?
7.For what purpose has a rocket motor a thrust termination system?
8.What does a guidance system determine?
9.Is the solid-propellant vehicle simpler than its liquid-pro pellant counterpart?
47.Прочтите и переведите без словаря:
Some Characteristics of Guided Missile Components
All guided missiles must contain certain components in order to perform their functions. The missile must have a body
or basic structure; it must |
be propelled; it must |
be guided; and |
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it must carry |
a payload. |
The main |
structure |
of the |
missile, |
which contains |
the other |
components, |
is called |
the |
airframe. |
The component which moves the airframe is the propulsion system, or power plant. The component which makes the vehicle a real guided missile is the guidance system. If the missile is to
31
perform a military task, it must contain a payload consisting |
of |
|
a warhead and fuzes. |
of the body |
of |
The airframe of a guided missile may consist |
||
the weapon and the airfoils 1 which stabilize it |
in flight and |
control its path. We know the missile airframe to serve the same purpose as the airframe of an ordinary airplane: it carries the
necessary components and determines the |
flight |
characteristics |
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of the vehicle. |
configuration — the shape and size |
of the airfra |
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The missile |
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m e— must be |
the following: |
1. |
The body |
and airfoils must |
be |
|
aerodynamically suitable for |
the |
speed at |
which |
the missile |
is |
to fly. 2. The airframe must be light in weight and sufficiently strong to withstand 12 great shock loads, vibrations, and accelera tions of high-speed flight. 3. The airframe must be easy to assem ble and to disassemble. The main components must form indepen-
'dent units. 4. The sections of the airframe must be simple in structure and easily fabricated. The sections are to be construe-, ted of material which is easy to work.
1airfoils — аэродинамические поверхности
2to withstand — выдерживать
48, Прочтите и переведите со словарем:
Propellant and Combustion Chamber
A considerable space in |
the rocket is naturally occupied by |
the propellant storage tanks |
compartment. The more fuel the |
rocket has, the farther it flies. The propellant stock of-the longrange modern missiles amounts to 80 per cent or more of their initial launching weight.
We know the propellant to consist of fuel and oxidizer. In normal conditions, in th$ furnace of a ship or locomotive for instance, the burning process is maintained by use of the oxygen in the air. This is practically non-existent at high altitudes. Therefore the rocket has to be provided with an oxidizer. Liquid oxygen or mixtures of “strong” nitric acid with special additives can be used for this purpose. Kerosene of various grades, alco
hols and other substances are used as fuel. It should |
be |
noted |
|||
that the rocket carries much more |
oxidizer |
than |
fuel. |
This can |
|
be seen from the following ratio: |
14.8 kg |
of air, |
or |
5.5 |
kg of |
nitric acid, or 3.37 kg of liquid oxygen is required for complete combustion of 1 kg of kerosene.
The engineers consider the heart of the rocket to be its engine with the combustion chamber. This is a very powerful heating machine in which the fuel’s chemical energy is transformed into the kinetic energy of the gas jet. Its speed reaches 2.2-2.7 km/sec. As a .result a jet force is generated which easily carries a rocket to great distances.
Each second several hundred kilogrammes of fuel and oxidizer are injected into the combustion chamber through special injectors. This work is performed by a special assembly, called turbopump unit, located between the propellant storage tanks and the combustion chamber.
When the engine is in operation, the pressure inside the chamber may reach 50—60 atmospheres and the temperature 3,000—3,500° C. How can the materials withstand such a fantas tic temperature? The designers found a very clever solution for this. The. combustion chamber is double-walled, much like the cooling jacket of an automobile engine. Only instead of water,
one of the propellant components flows into |
it. It |
takes heat |
from the chamber walls and thus is preheated |
and |
delivered to |
the injectors. |
|
|
Modern rockets are now equipped with solid-propellant engi nes as well. A solid mixture of fuel and oxidizer prepared in the form of blocks is filled into the rocket body, which in this case works as the combustion chamber.
2 П. И. Старостин
УРОК 4
Г р а м м а т и к а : |
Сложное подлежащее (§ 7) |
Т е к с т : |
Rocket Engine |
|
ПРЕДТЕКСТОВЫЕ |
УПРАЖНЕНИЯ |
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49. |
Прочтите |
и переведите, |
обращая |
внимание |
на |
перевод |
сложного |
||||||
подлежащего: |
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1. |
The nozzle |
is |
considered |
to |
be that |
part |
of |
the |
rocket |
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motor in which gases are accelerated to high velocities. 2. A |
|||||||||||||
modern rocket |
is known to be a complex mechanism consisting |
||||||||||||
of thousands of different parts. 3. |
Satellites |
launching |
rocket |
||||||||||
systems are known to have usually three or four stages. 4. The |
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payload is known to move along |
a free-flight path |
without |
|||||||||||
further expenditure of energy. 5. All the systems of the Salyut 4 |
|||||||||||||
were reported |
to function |
normally during |
the |
flight |
of |
the |
|||||||
station. |
6. Jet |
propulsion |
systems |
are |
thought |
to |
be |
reaction |
|||||
motors because |
they |
operate on |
the |
reaction principle. 7. The |
|||||||||
designers were |
said |
to |
usethe |
same |
principle |
of |
retrieving |
instrumentation. 8. The rocket is expected to drop smoothly to the Earth. 9. The steering device is thought to be an integral part of any guided missile. 10. The Moon is known to be the largest satellite of the solar system. 11. Single-stage rockets proved to be a means for launching payloads into a simple trajectory. 12. This satellite is certain to supply information on the earth radiation. 13. Three or more stages appeared to be necessary to achieve the required velocities to launch a minimum mass. 14. This propellant seemed to be suitable for a rocket engine. 15. This device turned out to be used in the latest designs of rockets. 16. The rocket engines are known to be divided into the main classes — the solid-propellant engines and the liquidpropellant engines. 17. Guided missiles are known to be divided into several classes depending on their launching method and type of the target, lfc. In modern long-range ballistic missiles
34
guidance is known to be achieved by a combination of gyrosco pes. 19. The design of a rocket propulsion is supposed to be influenced by many factors.
50. Прочтите слова и словосочетания:
to rely [ri'laij, relies upon this vehicle ['vi:ikl]; to eject [i:'d3ekt], ejection, by ejection of matter; original [э'пс^эп!), originally, originally carried within the vehicle; super, ['sjurpaj, supersonic ['sjuipa'somk], a supersonic stream, a supersonic
exhaust stream; either |
['aiba], either solid or liquid; a combustion |
||
[kom'bAst/anJ, a combustion chamber; to |
oxidize |
['oksidaiz], |
|
an oxidizer, to burn in |
an oxidizer; separate |
['seprit], |
a separate |
chamber ['t/eimbo], a separate combustion chamber; molecules
j/molikju:lzJ, molecules of the gas; to |
possess fpa'zes], to |
possess large amounts of energy; uniform |
['ju:mfo:m], uniformly, |
uniformly directed |
|
TEXT |
|
ROCKET ENGINE |
|
Propulsion for a ballistic vehicle usually relies upon a rocket system which is defined as propulsion by ejection of matter, all of which is originally carried within the vehicle which is being propelled. A rocket engine is known to produce an unbalanced force on the vehicle and is thus able to move it. The propulsive action of the rocket engine arises from the reaction to the acceleration, relative to the rocket engine, of a mass of propel lant originally carried within the rocket-propelled vehicle. In the rocket engines which are employed in ballistic missiles, accelera tion of the propellant mass is brought about by:
(a)releasing heat energy by a chemical reaction of propel lants within a combustion.chamber, and
(b)the use of an expansion nozzle to produce a supersonic
exhaust stream by expanding the evolved gas from combustionchamber pressure to ambient pressure.
The combustion chamber and expansion nozzle are together
known as the thrust chamber. |
rocket |
vehicles |
can |
be stored |
Propellants which are used in |
||||
in either solid or liquid form, and |
rocket |
engines |
are |
considered |
to be solidor liquid-propellant rocket engines respectively. The propellant tanks which are usually integral with the structure of the missile contain the propellants before their injection into the combustion chamber.
A rocket engine acts as a chamber containing a high-pressure gas which is continuously replenished as some of the gas escapes through an orifice into the region of lower pressure outside the
chamber. The |
simplest rocket engine proves to |
consist of |
a |
chamber — the |
combustion chamber -^-.in which |
fuel can |
be |
о* |
|
|
35 |
|
|
|
burned in an oxidizer. The oxidizer can be carried either separately as in liquid propellants or mixed with the fuel as with solid propellants. The fuel and oxidizer are known as propel lants. In a liquid-propellant engine they are injected into the combustion chamber. In. a solid-propellant motor, the propellant storage tank and the combustion chamber are one and the same.
The |
propellant |
mixture is |
triggered |
electrically, |
thermally, |
or |
chemically, to |
produce a heat-releasing chemical |
reaction, |
and |
|||
the |
molecules |
of the gas |
produced |
by the combustion process |
possess large amounts of energy, moving rapidly in all directions
within |
the chamber. Individually these molecules have |
a high |
||||
kinetic |
energy .but |
their motions |
are randomly |
directed. |
To |
|
achieve |
a propulsive |
effect, this |
random motion |
has |
to |
be |
directed as uniformly as possible, in a direction away from the thrust chamber.
In exhausting through the expansion nozzle, the random motion of the gas particles is changed to a more directional motion. The gas emerges as a high-velocity stream from the thrust chamber.
The four components of a liquid-propellant engine are: 1 ) the feed system which is used to move jthe propellants from their storage tanks into the combustion chamber, 2 ) the thrust chamber where the propellants are burned and then expelled at
high |
velocity, 3) a control system |
which |
starts, stops and |
|
controls |
the operation of the engine, |
and 4) |
auxiliary devices |
|
such |
as |
means to deflect the jet to change the direction of the |
||
thrust |
vector. |
|
|
Слова и словосочетания для запоминания
п |
combustion |
chamber, ejection, expansion nozzle,, feed |
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v |
system, orifice, region, stream, thrust chamber |
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arise |
(arose; arisen), |
bring |
about |
(brought; brought), |
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emerge, escape, evolve, expel, inject, possess, propel, |
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a |
release, replenish, store, trigger |
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ambient, random, supersonic |
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adv respectively, |
uniformly |
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prep outside |
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УПРАЖНЕНИЯ |
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||
в |
51. |
Прочтите |
и переведите, обращая внимание па перевод инфинитива |
|||
перфектной форме, |
являющегося |
часгыо |
сложного |
подлежащего:1 |
1 . This satellite was reported to have supplied information on the general structure of the ionosphere. 2 . In recent years the Soviet Union is known to have investigated the radio waves emitted by the Moon on frequencies within the range of 13—
35 cm. 3. Soviet scientists are considered to have done much for
36
the development of astronautics. 4. World meteorological centers are known to have been set up in Moscow and Washington and a direct communication channel has been established between them. 5. Two servo systems were considered to have been used during the powered flight to control position and velocity of this ballistic missile.. 6. The design of a rocket propulsion is believed to have been perfected.
52. Прочтите. Укажите номера предложений, содержащих инфинитив — часть сложного подлежащего. Переведите все предложения:
1. Propellants which are used in rocket vehicles are believed to be stored in either solid or liquid form. 2. The liquid rocket engine is known to consist of the combustion chamber, the feed system and the control system. 3. The turbojet engine is employ ed to propel certain guided missiles and aircraft in the high subsonic speed range. 4. We know the combustion chamber to be cooled by the oxidizer passing through a coolant space before
injecting into |
the combustion chamber |
through |
a catalyzer. |
5. The present |
propulsion is considered |
to employ |
the energy |
developed from combustion of fuel with the oxidizer. 6. A num ber of messages were known to be sent to the satellite where they were recorded and returned to the Earth at various points within the range of its radio-transmitters. 7. The observers are trained to recognize every object in the sky which they will see during the period of about 2 hours. 8. The orbits of the Soviet and American satellites are reported to be inclined approximately 25° to the polar plane. 9. Modern radar systems prove to be able to indicate the velocity of the aircraft with respect to the earth’s surface. 10. We were recommended to record the observations with the exact time of the passage of the satellite. 11. Some of the gas is certain to escape through an orifice into the region of lower pressure outside the chamber. 12. The thrust chamber is considered to be cooled by the passage of fuel through many, tubes making up its walls. 13. Rocket and missile development since 1930 is known to have resulted in launching instrumenta tion and manned vehicles into space. 14. They suppose most modern rocket motors to employ regenerative cooling in which the fuel must circulate around the combustion chamber and nozzle before it is injected for burning. 15. The speed of the reaction is found to be affected by the temperature of the propellant and the ambient temperature. 16. This satellite was designed to supply information on the general structure of the ionosphere. 17. The jet velocity of a rocket engine is considered to be the velocity at which the gases are ejected from the nozzle. 18. A missile is to be designed for the trajectory which it is expected to follow. 19. The powered flight of the ballistic missile appears to depend upon the energy that must be imparted to the payload.
37
53. Прочтите. Укажите номера предложений, в которых выделенное сло во является сказуемым. Переведите все предложения:
1 . |
The |
analysis of these |
data |
means that |
all |
the |
systems |
|
function normally. 2. These devices are the auxiliary means for |
||||||||
feeding the propellant into the combustion chamber. 3. |
The |
|||||||
development of entirely new compatible means of spaceships |
||||||||
docking |
is the |
problem of |
greatest importance. 4. |
This means |
||||
that if a man exerts a force of 150 pounds on the car, the car |
||||||||
exerts an equal and opposite force of |
150 pounds |
bn |
the |
man. |
||||
5. An important means of man’s penetration into near space is |
||||||||
the setting-up |
and flight |
of |
orbital |
scientific |
stations |
with |
rotating crews. 6. A ballistic missile flies the greater part of its trajectory as a freely thrown body; this means that it is acted upon only by two forces: the earth’s gravitation and the resistance
of the |
air. 7. Propellants rich in hydrogen and other light |
||
elements are advantageous because they lead to a low mean |
|||
molecular weight of the exhaust gas. |
|
||
54. |
Прочтите и переведите, |
обращая ' внимание |
на перевод союза |
“either... |
or”: |
|
|
1 . |
Propellants which |
are used in rocket |
vehicles are known |
to be stored in either solid or liquid form. 2. Launching of a missile is carried out either from-open ground emplacements or from underground silos. 3. The release of heat away from the vehicle can* be accomplished'either by the action of strong shock waves or by radiation .of heat away from the hot surface of the vehicle. 4. Short-range missiles may be used against either fixed or moving targets. 5. Such satellite can contain either television cameras or photographic equipment for transmitting pictures to the Earth. 6. The oxidizer can be carried either separately as in liquid propellants or mixed with the fuel as with solid propel
lants. |
7. |
The spaceship |
is |
controlled |
either |
automatically or |
||||||||
manually by the cosmonaut. |
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55. |
Определите |
по |
суффиксам, |
к каким частям |
речи |
относятся |
слова, |
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и переведите их: |
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1 . |
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oxidizer; 2. oxidation; 3. injection; 4. injector; 5. superso |
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nic; 6. |
respective; |
7. |
respectively; |
8. |
uniformly; 9. |
ejection;* |
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1 0. storage; |
1 1 . expansion; 1 2 . propulsive |
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56. |
Прочтите и |
переведите,. обращая-' внимание на |
значение |
отрицатель |
||||||||||
ного префикса "un-”:1 |
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1 . balanced, |
unbalanced; |
2 . |
distributed,, |
undistributed; |
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3. desirable, undesirable; 4. reliable, unreliable; 5. accomplished, |
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unaccomplished; 6. achievable, unachievable; 7. attached, |
unat |
|||||||||||||
tached; |
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8. |
available, |
unavailable; |
9. |
changed, |
unchanged; |
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1 0. restricted, unrestricted; |
1 1 . usable, |
unusable; |
1 2 . successful, |
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unsuccessful |
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38
57. К каждому словосочетанию подберите русский эквивалент:
1 . to bring about the accele |
1 . воспламенять |
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топливную |
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|
ration of |
the |
.propellant |
|
смесь |
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mass |
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2. выбрасываться |
через |
соп |
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2 . to use a feed system |
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3. to |
replenish the |
storage |
3. |
ловое отверстие |
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камера |
ракетного двига |
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4. |
tanks |
the |
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' |
4. |
теля |
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тепловую |
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outside |
combustion |
высвобождать |
|
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5. |
chamber |
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5. |
энергию |
|
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сверхзвуко |
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ejection of matter |
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производить |
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вую струю |
выхлопных га |
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6. to propel a rocket |
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зов |
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распределен |
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6. равномерно |
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7. to |
produce |
a |
supersonic |
7. |
ный окислитель |
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|
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сверхзвуковое сопло |
|
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exhaust |
stream |
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8. вызывать |
ускорение |
мас |
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8. a thrust chamber |
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9. to escape through an ori |
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сы топлива |
в движение |
ра |
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9. приводить |
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fice |
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кету |
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вещества |
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10. a random motion |
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10. выбрасывание |
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1 1 . to |
release heat |
energy |
И. вне камеры сгорания |
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1 2 . an expansion nozzle |
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12. пополнять топливные баки |
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13. |
a |
uniformly |
distributed |
13. |
беспорядочное движение |
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14. |
oxidizer |
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the |
propellant |
14. |
использовать |
систему |
по |
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to |
trigger |
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mixture |
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дачи (топлива) |
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58. |
Прочтите и переведите без словаря: |
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|||||
|
1 . |
to' |
expel |
the |
gas from a |
combustion chamber; 2. the |
|||||||
propellant |
mixture |
triggered |
electrically; |
3. |
the |
randomly |
directed motions; 4. to possess high kinetic energy; 5 an ambient pressure; 6. to arise from the reaction to the acceleration; 7. to employ an expansion nozzle; 8. the respectively changing thrust; 9. to bring about a supersonic stream; 10. to expel gases at high velocity; 1 1 . a region of lower pressure; 12. the gas emerged as a high velocity stream from the thrust chamber
59. ГТрочтите и переведите без словаря:
1. The propellant mixture is triggered and produces a heatreleasing chemical reaction. 2. The random motion of molecules
has to be directed as uniformly as possible. 3. An expansion ^nozzle is known to be. used to produce a supersonic exhaust stream. 4. The propellants must be stored in either solid or liquid form. 6. The storage tanks are replenished from time to time; 6. The gas is expected to escape through an orifice into the
39
region of lower pressure. 7. In a liquid-propellant engine the propellants are injected into the combustion, chamber. 8. These molecules seem to possess great amount of energy.
60. Найдите в тексте "Rocket Engine" ответы на вопросы:
1. What is'acceleration of the propellant mass in the rocket engines brought about by?
2. In what form can propellants in rocket vehicles be stored?
3.How can the oxidizer be carried?
4.What motion is the random motion of the gas particles changed to in exhausting through the expansion nozzle?
5. How many basic components of a liquid rocket engine are there?
6.How is the propellant mixture triggered?
7.What reaction does the propulsive action of the rocket engine arise from?
8.Are the combustion chamber and expansion nozzle together known as the thrust chamber?
61.К каждому слову подберите русский эквивалент:
1. |
solid |
1. обладать |
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2. to bring about |
2. |
агрегат |
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3. to |
propel |
3. |
окислитель |
|
4. |
region |
4. |
в отношении |
|
5. |
to |
desire |
5. |
выделять |
6. |
to |
store |
6. |
сообщать |
7. |
airframe |
7. |
появляться |
|
8. to emerge |
8. |
возникать |
||
9. control |
9. |
выбрасываться |
||
10. respectively |
10. |
приводить в движение |
||
11. to impart |
И. окружающий |
|||
12. |
to evolve |
12. |
неотъемлемый |
|
13. |
assembly |
13. |
корпус {ракеты) |
|
14. |
to escape |
14. |
желать |
|
15. |
to |
arise |
15. |
управление |
16. |
oxidizer |
16. |
вызывать |
|
17. |
ambient |
17. |
хранить |
|
18. |
in respect (to) |
18. |
твердый |
|
19. |
to |
possess |
19. |
соответственно |
20. |
integral |
20. |
область |
62. Прочтите и переведите без словаря:
General Characteristics of the Turbojet Engine
This engine is known to consist of a diffuser *, a mechanical compressor, a combustion chamber, a mechanical turbine, and an exhaust nozzle. The function of the diffuser is to transform
40